\"\"

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The atmospheric pressure is \"\" and altitude is \"\".

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The rate of change of \"\" with respect to \"\" is proportional to \"\".

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\"\"

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Hence \"\", where \"\" is a constant.

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At the sea level, the pressure is \"\" kpa.

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Pressure at an altitude of \"\" is \"\" kpa.

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The general equation is \"\".

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Substitute \"\"  and \"\" in the above equation.

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\"\"

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Substitute \"\" in the \"\".

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Pressure at an altitude \"\" is \"\".

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\"\"

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(a).

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Find the pressure at a altitude of \"\".

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Substitute \"\" in the pressure function \"\".

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\"\"

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The pressure is \"\" kpa at an altitude of \"\".

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\"\"

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(b).

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Find the pressure when altitude is \"\" m.

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Substitute \"\" in the equation \"\".

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\"\"

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The Pressure is \"\" kpa when altitude is \"\" m.

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\"\"

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(a) The pressure is \"\" kpa at an altitude of \"\".

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(b) The Pressure is \"\" kpa when altitude is \"\" m.